Effect of ply angle misalignment on out-of-plane deformation of symmetrical cross-ply CFRP laminates: Accuracy of the ply angle alignment
โ Scribed by Yoshihiko Arao; Jun Koyanagi; Shin Utsunomiya; Hiroyuki Kawada
- Publisher
- Elsevier Science
- Year
- 2011
- Tongue
- English
- Weight
- 467 KB
- Volume
- 93
- Category
- Article
- ISSN
- 0263-8223
No coin nor oath required. For personal study only.
โฆ Synopsis
This paper discusses the accuracy of ply angle alignment and how it relates to out-of-plane deformation in carbon fiber reinforced plastics (CFRP) laminates. We investigated the deformation of symmetrical cross-ply laminates under hot and humid conditions. In spite of the symmetrically stacked laminates, unpredictable out-of-plane deformation occurred over time due to ply angle misalignment. The deformation was unstable and disproportionate to the absorbed moisture. A Monte Carlo simulation based on laminate theory was performed to quantify the deformation induced by the ply angle misalignment. Symmetrical cross-ply laminates were found to twist as they absorbed water when they underwent ply angle misalignments. By comparing the analytical results with experimental results, we concluded that a standard deviation of approximately 0.4ยฐexists as ply angle misalignment in the laminates used in this study and that this slight ply angle misalignment can be a significant factor in out-of-plane deformation of cross-ply laminates.
๐ SIMILAR VOLUMES
This paper presents studies of the global nominee deflection and ~tbuc~ing behavior of symmetric angle-ply iaminated plates. A new transformation between on-axis and off-axis moduhrs is established to make a link between the stiffness of angle-ply plates and the global constants in orthotropic trans
The in-plane free vibrational analysis of symmetric cross-ply laminated circular arches is studied using both the Timoshenko and Bernoulli}Euler beam theories. The free vibration equations are derived based on the distributed parameter model. The transfer matrix method is used in the analysis. The n
In this study, the stiness method solution based on the ยฎrst order shear deformation theory is used for the purely out-of-plane (out-of-plane bending and torsional) free vibration analysis of symmetric cross-ply laminated beams. A beam element has six degrees of freedom. The inยฏuence of the rotary i